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Missile guidance laws for a strapdown seeker with a narrow field-of-view : 좁은 화각을 갖는 스트랩다운 탐색기를 위한 유도기법

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dc.contributor.advisor최진영-
dc.contributor.author이채흔-
dc.date.accessioned2017-07-13T07:00:33Z-
dc.date.available2017-07-13T07:00:33Z-
dc.date.issued2013-08-
dc.identifier.other000000013891-
dc.identifier.urihttps://hdl.handle.net/10371/118949-
dc.description학위논문 (박사)-- 서울대학교 대학원 : 전기·컴퓨터공학부, 2013. 8. 최진영.-
dc.description.abstractNew guidance laws are proposed to solve the problem of when a missile is equipped with a strapdown seeker instead of a gimbaled seeker. The strapdown seeker has advantages of relatively simple implementation compared to a gimbaled seeker, and it can eliminate frictional cross-coupling significantly save on costs. There have been many studies to enable guided missiles to use strapdown seekers, but they have several weaknesses, such as measurement error caused by scale factor error, radome errors, glint noise, narrow field-of-view (FOV), and so on. Among these weak points, focus is centered on the narrow FOV of the strapdown seeker.
A hybrid guidance (HG) law is proposed to maintain the lock-on condition in spite of the narrow FOV of the strapdown seeker. The proposed HG law consists of two guidance phases, which assume operation at a switching boundary. In the first phase, the proportional navigation guidance (PNG) law is applied during the time when the look angle is inside the switching boundary. For the second phase, when the look angle is outside the switching boundary, a new guidance law is derived to keep the look angle within the FOV by employing a Lyapunov-like function based on sliding-mode control methodology. The appropriate determination of the switching boundary is an important issue. The idea behind selecting the switching boundary is to use the PNG law as much as possible, and to make the missile stay in the lock-on condition.
A lock-on guidance (LOG) is proposed as another approach to solve the problem of narrow FOV, based on the concept of the pursuit guidance (PG) law. In order to derive the LOG law, we use a Lyapunov-like function based on the sliding-mode control methodology. An advantage of the LOG law is that a missile guided by the LOG law can intercept a target with a very narrow FOV of the strapdown seeker. Because such a seeker often has to be implemented for more accurate measurements, this kind of guidance law is needed to prepare for such a situation. The LOG law is simple and has good performance against a target with high speed.
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dc.description.tableofcontentsAbstract i
Contents iii
List of Figures vi
List of Tables x

Chapter 1. Introduction 1
1.1 Background and Motivations 1
1.2 Contents of the Research 6

Chapter 2. Preliminary Survey 10
2.1 Survey on Guidance Laws 10
2.1.1 Classical Guidance Laws 10
2.1.1.1 Pursuit Guidance Law 12
2.1.1.2 Constant Bearing Course Guidance Law 13
2.1.1.3 Line-of-Sight Guidance Law 13
2.1.1.4 Proportional Navigation Guidance Law 16
2.1.2 Modern Guidance Laws 23
2.1.2.1 Optimal-Control-Based Guidance Law 24
2.1.2.2 Predictive Guidance Law 27
2.1.2.3 Game-Theory-Based Guidance Law 30
2.1.2.4 Sliding-Mode-Control-Based Guidance Law 31
2.1.3 Summary 32
2.2 Survey on Missile Seekers 33
2.2.1 Gimbal Seeker 34
2.2.2 Strapdown Seeker 35
2.2.3 Summary 36
2.3 Remarks and Discussions 37

Chapter 3. The Proposed Guidance Laws 40
3.1 Hybrid Guidance Law 40
3.1.1 Problem Statement 41
3.1.2 The Overall Scheme 46
3.1.3 Guidance Law for the First Phase 48
3.1.4 Guidance Law for the Second Phase 48
3.1.5 Switching Boundary Estimation 50
3.2 Lock-on Guidance Law 56
3.2.1 Problem Statement 57
3.2.2 The Overall Scheme 62
3.2.3 Derivation 64

Chapter 4. Simulation Results 70
4.1 Hybrid Guidance Law 70
4.1.1 Non-maneuvering Target 70
4.1.2 Maneuvering Target 76
4.2 Lock-on Guidance Law 85
4.1.1 Non-maneuvering Target 85
4.1.2 Maneuvering Target 96
4.3 Comparison of Hybrid Guidance Law and Lock-on Guidance Law 105

Chapter 5. Conclusions 109
5.1 Concluding Remarks 109
5.2 Further Study 111

Bibliography 112

국문초록 123
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dc.formatapplication/pdf-
dc.format.extent2545236 bytes-
dc.format.mediumapplication/pdf-
dc.language.isoen-
dc.publisher서울대학교 대학원-
dc.subjectField of View-
dc.subjectHybrid Guidance Law-
dc.subjectLock-on Guidance Law-
dc.subjectPursuit Guidance-
dc.subjectProportional Navigation Guidance-
dc.subjectSliding-Mode Control-
dc.subjectStrapdown Seeker-
dc.subjectSwitching Boundary-
dc.subject.ddc621-
dc.titleMissile guidance laws for a strapdown seeker with a narrow field-of-view-
dc.title.alternative좁은 화각을 갖는 스트랩다운 탐색기를 위한 유도기법-
dc.typeThesis-
dc.description.degreeDoctor-
dc.citation.pagesi, 124-
dc.contributor.affiliation공과대학 전기·컴퓨터공학부-
dc.date.awarded2013-08-
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